|Publication number||US7374137 B2|
|Application number||US 11/326,589|
|Publication date||May 20, 2008|
|Filing date||Jan 4, 2006|
|Priority date||Jan 4, 2006|
|Also published as||US20070152124, WO2007079474A2, WO2007079474A3|
|Publication number||11326589, 326589, US 7374137 B2, US 7374137B2, US-B2-7374137, US7374137 B2, US7374137B2|
|Original Assignee||Wayne Staney|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (30), Referenced by (28), Classifications (59), Legal Events (2)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The present invention relates to a field of support structures and, more particularly, to a support structure for solar panel collectors, satellite antennas and other objects that need to be fixed toward a point in space.
Solar panels and satellite antennas are directed to a particular point in space to be effective. A solar panel collector must either be directed toward the sun where it will be most effective or made to track the sun as it moves across the sky. Solar panels are used to collect energy from the Sun and require optimum positioning whether the energy is for heating of water or providing electrical power. The weight of the panels is dependant upon the panel size but can be quite heavy if the solar panel includes circulating water.
Satellite antennas, both flat and parabolic, can be found throughout the world for communication purposes. These antennas must also be directed to a particular point in space to be effective. Solar panels and satellite antennas both require support structures capable of adjustment yet capable of inhibiting all movement even if presented with high winds.
One of the problems with the prior art support structures is their inability to both precisely hold large directional objects while allowing for ease of adjustment. For instance, if a solar panel is designed to be fixed, as opposed to tracking, a necessity for the safety of the installers is paramount. This need arises as conventional support structures place a burden upon the installer to prevent damage during directional positioning. Prior art devices have not disclosed the necessity for a support structure capable of withstanding extremely high winds from causes such as hurricanes. Such high winds can cause misadjustment if the panel moves even one inch.
Thus, what is lacking in the art is a heavy duty directional support structure capable of holding large heavy panels yet provide ease in directionally pointing by allowing the installer to rotate and tilt the directional panel as necessary.
Set forth is a directional support structure for use with solar panels, flat or raised satellite antennas, and the like structures required to be directionally facing a fixed point in space. The directional support structure includes an adjustable bracket that allows for pivoting of the mounting plate even when the mounting plate is loaded with solar panels or satellite panels, despite the weight of such devices. Rotational or azimuth movement is maintained by use of a mounting bracket secured to a base member that allows rotation with operator safety in mind by eliminating disengagement of the directional devices once they are secured to the mounting plate. Upon proper rotational placement, flanges are fastened together sandwiching a flaring located on the lower end of the mounting bracket thereby preventing further rotational movement. An adjustment bracket is provided to allow latitude adjustment of the mounting plate by use of turn buckles that provide precise adjustment and absolute rigidity upon locking of the turn buckles. A base member includes a hollow column that can be placed in the ground or bolted on a fixed structure. The column is hollow to provide a wire chase for concealment of pipes and/or electrical wiring.
Thus, an objective of the instant invention is to disclose a directional support structure capable of azimuth and latitude adjustment despite the weight of the devices to be directionally positioned.
Yet another objective of the invention is to provide a support structure that provides a safe structure for installers by creating a rigid mounting base that allows for positional adjustment.
Still another objective of the instant invention is to provide an industrial stand capable of withstanding weather extremes such as hurricane winds, without movement of the positioning elements.
Still another objective of the instant invention is to disclose the use of a universal mounting plate capable of holding a plurality of solar panel basins.
Still another objective of the instant invention is to disclose the use of solar panel basins that allow for the flush mount of solar panels to protect from side wind lifting.
Still another objective of the instant invention is to teach the use of a mounting plate that can be used for devices that require directional placement including satellite antenna panels.
The above-stated objectives as well as other objectives not specifically stated, are within the scope of the present invention, and will become apparent from the Derailed Description of the Invention, Drawings, and Claims.
Detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention which may be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriate structure.
Referring now to
The base member 32 is formed from a hollow upright column 34 defined by an upper end 36 spaced apart from a lower end 38 a distance to allow clearance of the mounting plate 12 from contacting an object when a solar panel or antenna is placed thereon. This is particularly helpful when the base member is mounted on the ground wherein the mounting plate extends up over the ground a distance which will handle most average snow falls, and allows shrubbery or other lawn items to be placed around the base without interfering with the solar panel and or satellite antenna reception.
Referring now to
In a preferred embodiment the first flange 42 includes a receptacle 50 sized to cooperate with the flare 40, thereby capturing the flare in a fixed position. Alternatively, referring to
Now referring to
It should be understood that the foregoing relates to only preferred embodiments of the present invention, and that it is intended to cover all changes and modifications of the embodiment of the invention herein used for the purposes of disclosure, which do not institute departures from the spirit and scope of the invention.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US3593954 *||Jun 4, 1970||Jul 20, 1971||Kofabco Inc||Swivel connection for a chair|
|US3714660||Jul 23, 1970||Jan 30, 1973||Itt||Antenna mounting structure|
|US3940771||Apr 21, 1975||Feb 24, 1976||Rockwell International Corporation||Variable angle support apparatus|
|US4126865 *||Nov 11, 1976||Nov 21, 1978||The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland||Satellite tracking dish antenna|
|US4138991 *||Jul 27, 1977||Feb 13, 1979||Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft-Man||Flat solar collector|
|US4232320||Apr 21, 1978||Nov 4, 1980||Andrew Corporation||Mount for earth station antenna|
|US4251819||Jul 24, 1978||Feb 17, 1981||Ford Aerospace & Communications Corp.||Variable support apparatus|
|US4300537||Sep 19, 1980||Nov 17, 1981||Davis Thomas A||Solar panel mount|
|US4545557||Jul 22, 1983||Oct 8, 1985||Rogers Bernard J D||Articulated mounting means for poles, antennas and the like|
|US4617572 *||Aug 14, 1984||Oct 14, 1986||Albert Hugo||Television dish antenna mounting structure|
|US4783662||Feb 18, 1986||Nov 8, 1988||Delta Satellite Corportion||Polar mount for satellite dish antenna|
|US4799064 *||Apr 27, 1987||Jan 17, 1989||Tsubakimoto Chain Company||Gyratory parabolic antenna driving device|
|US4799642||Feb 3, 1987||Jan 24, 1989||Rt/Katek Communications Group, Inc.||Antenna mounting|
|US4819006 *||May 8, 1986||Apr 4, 1989||Aluminum Company Of America||Mount for supporting a parabolic antenna|
|US4819007 *||Jun 22, 1987||Apr 4, 1989||Andrew Corporation||Supporting structure for reflector-type microwave antennas|
|US4895990 *||Jun 24, 1987||Jan 23, 1990||I.S.C. Chemicals Limited||Fluorinated polycyclic compounds|
|US4918363 *||Sep 30, 1988||Apr 17, 1990||Venture Mfg. Co.||Actuator for TVRO parabolic antenna|
|US4922264||Apr 24, 1989||May 1, 1990||Fitzgerald Robert M||Satellite antenna mounting apparatus with ballast means|
|US5007560 *||Mar 1, 1989||Apr 16, 1991||Sassak John J||Beer dispensing and monitoring method and apparatus|
|US5075682 *||Mar 30, 1990||Dec 24, 1991||Dehnert Douglas K||Antenna mount and method for tracking a satellite moving in an inclined orbit|
|US5355145 *||Jul 30, 1992||Oct 11, 1994||Lucas Donald E||Satellite dish actuator mounting construction|
|US5512913 *||Apr 14, 1994||Apr 30, 1996||Staney; Michael W.||Flat plate antenna, scaler collector and supporting structure|
|US5576722 *||Sep 13, 1994||Nov 19, 1996||The United States Of America As Represented By The Secretary Of The Army||Mobile satellite antenna base and alignment apparatus|
|US5614918||Jul 24, 1996||Mar 25, 1997||The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration||Global positioning system antenna fixed height tripod adapter|
|US5798517 *||Feb 3, 1997||Aug 25, 1998||Berger; Alexander||Sun tracker system for a solar assembly|
|US6037913 *||May 13, 1999||Mar 14, 2000||Johnson; Pamela Kay||Moveable satellite dish antenna mount|
|US6195066||Jan 15, 2000||Feb 27, 2001||Thomas C. Pegues, Jr.||Satellite dish mounting arm|
|US6284968||Jun 19, 2000||Sep 4, 2001||Joseph Z. Niesyn||Solar-tracking system|
|US20070052604 *||Oct 28, 2005||Mar 8, 2007||Seaspace Corporation||Antenna positioner system|
|US20070095993 *||Oct 26, 2006||May 3, 2007||Fumoto Giken Co., Ltd.||Moving apparatus|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US7793599 *||May 14, 2004||Sep 14, 2010||Pavel Truksa||Device for position locking of folding modular systems|
|US7871031 *||Mar 23, 2009||Jan 18, 2011||Tekpak Corporation||Device having a liftable strap supply reel|
|US8220744||Jul 17, 2012||Airbus Deutschland Gmbh||Fitting for introducing high forces into a fuselage cell of an aircraft|
|US8382038 *||Jan 11, 2008||Feb 26, 2013||Airbus Operations Gmbh||Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component|
|US8408492||Apr 2, 2013||Airbus Deutschland Gmbh||Floor panel for forming a loading area in a cargo hold of an aircraft|
|US8542156 *||Dec 15, 2009||Sep 24, 2013||Sea Tel, Inc.||Pedestal for tracking antenna|
|US8578928 *||Apr 27, 2009||Nov 12, 2013||Talleres Clavijo, S.L.||Directable solar panel systems|
|US8779278||Sep 23, 2010||Jul 15, 2014||Raytheon Company||Air supported photovoltaic system|
|US8794578 *||Apr 27, 2011||Aug 5, 2014||Wistron Neweb Corporation||Adjusting mechanism for adjusting rotary angle and antenna system therewith|
|US8866695 *||Feb 23, 2012||Oct 21, 2014||Andrew Llc||Alignment stable adjustable antenna mount|
|US8919961 *||Apr 30, 2013||Dec 30, 2014||Nelson Planting||Inflatable, pressure-controlled, portable line-concentrating heliostat|
|US9255725 *||Jan 30, 2014||Feb 9, 2016||Jasem M K Th Sh Al-Enizi||Sun tracking solar energy collection system|
|US9343592||Aug 1, 2011||May 17, 2016||Alion Energy, Inc.||Electrical interconnects for photovoltaic modules and methods thereof|
|US9352941||Mar 11, 2013||May 31, 2016||Alion Energy, Inc.||Gantry crane vehicles and methods for photovoltaic arrays|
|US20070163474 *||May 14, 2004||Jul 19, 2007||Pavel Truksa||Device for position locking of folding modular systems|
|US20080173755 *||Jan 15, 2008||Jul 24, 2008||Herrmann Benthien||Floor panel for forming a loading area in a cargo hold of an aircraft|
|US20100139741 *||Oct 12, 2009||Jun 10, 2010||Wares Brian S||Frame-Integrated Pivot Bearing For Solar Collector Assembly|
|US20100149059 *||Dec 15, 2009||Jun 17, 2010||Sea Tel, Inc (D/B/A Cobham Satcom Marine Systems||Pedestal for tracking antenna|
|US20100237182 *||Sep 23, 2010||Chin-Chang Liu||Device having a liftable strap supply reel|
|US20110108668 *||Jan 11, 2008||May 12, 2011||Hermann Benthien||Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component|
|US20110174295 *||Apr 27, 2009||Jul 21, 2011||Talleres Clavijo, S.L.||Directable solar panel systems|
|US20110266411 *||Nov 3, 2011||David Silverberg||Ergonomically balanced and moveable arm support system|
|US20120211624 *||Aug 23, 2012||Hung-Yuan Lin||Adjusting mechanism for adjusting rotary angle and antenna system therewith|
|US20130068275 *||Mar 15, 2012||Mar 21, 2013||Alion, Inc.||Systems and methods for mounting photovoltaic modules|
|US20130306135 *||Apr 30, 2013||Nov 21, 2013||Nelson Planting||Inflatable, pressure-controlled, portable line-concentrating heliostat|
|US20150211768 *||Jan 30, 2014||Jul 30, 2015||Jasem M K Th Sh Al-Enizi||Sun tracking solar energy collection system|
|CN103637660A *||Dec 4, 2013||Mar 19, 2014||昆明理工大学||Multifunctional hanging frame|
|CN103637660B *||Dec 4, 2013||Mar 30, 2016||昆明理工大学||一种多功能挂架|
|U.S. Classification||248/122.1, 16/286, 108/9, 403/337, 248/291.1, 403/261, 108/8, 343/878, 248/121, 248/425, 248/125.1, 248/415, 343/880, 248/292.12, 248/125.7, 403/336, 248/123.11, 248/372.1, 248/284.1, 343/882, 248/354.1, 248/292.13, 248/419, 343/883, 248/292.11, 108/10, 343/892, 16/290, 343/765, 248/516, 248/125.2, 108/145, 343/757, 403/335, 108/6, 248/371|
|International Classification||A47F5/00, F16M13/00, A47F7/00, F16M11/00|
|Cooperative Classification||Y10T403/64, Y10T403/645, Y10T16/5383, Y02E10/47, F24J2/541, Y10T403/642, F16M11/10, Y10T403/4688, F24J2002/5465, F16M11/12, F24J2/523, H01Q1/1264, F16M11/2014, Y10T16/53835|
|European Classification||F16M11/20A1, H01Q1/12E2, F16M11/12, F16M11/10, F24J2/54B4|
|Nov 18, 2011||FPAY||Fee payment|
Year of fee payment: 4
|Nov 20, 2015||FPAY||Fee payment|
Year of fee payment: 8